CN217802060U - Numerical control vibration knife and crossbeam belt and aircraft nose dolly connection guiding mechanism thereof - Google Patents
Numerical control vibration knife and crossbeam belt and aircraft nose dolly connection guiding mechanism thereof Download PDFInfo
- Publication number
- CN217802060U CN217802060U CN202221368560.9U CN202221368560U CN217802060U CN 217802060 U CN217802060 U CN 217802060U CN 202221368560 U CN202221368560 U CN 202221368560U CN 217802060 U CN217802060 U CN 217802060U
- Authority
- CN
- China
- Prior art keywords
- connecting plate
- crossbeam
- belt
- aircraft nose
- dolly
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Connection Of Plates (AREA)
Abstract
The utility model relates to a numerical control vibrates sword and guiding mechanism is connected with the aircraft nose dolly to crossbeam belt thereof. This numerical control vibrating knife, including aircraft nose dolly and crossbeam, the aircraft nose dolly is located crossbeam one side and moves along crossbeam length direction, the crossbeam belt is rectangular form, and be the annular around the crossbeam, numerical control vibrating knife still includes crossbeam belt and aircraft nose dolly connection guiding mechanism, it includes the connecting plate to connect guiding mechanism, two fixed blocks, locating plate and adjusting bolt, two fixed blocks respectively with the both ends fixed connection of crossbeam belt, the connecting plate is located between two fixed blocks, the one end and the aircraft nose of connecting plate get off fixed connection, the connecting plate is along crossbeam belt length direction guide cooperation with two fixed blocks respectively, locating plate fixed connection is on the connecting plate, adjusting bolt bolted connection is on the locating plate, adjusting bolt's screw rod section and connecting plate screw-thread fit. The utility model discloses a reliable fixed connection of aircraft nose dolly and crossbeam belt is made to connecting plate, fixed block to easy dismounting.
Description
Technical Field
The utility model belongs to the technical field of numerical control vibration sword, concretely relates to numerical control vibration sword and guiding mechanism is connected with the aircraft nose dolly to crossbeam belt thereof.
Background
With the rapid development of scientific technology and the rapid increase of the labor cost of society, a plurality of cutting machines capable of replacing most of the traditional manual cutting operation of flexible materials are correspondingly provided on the market, and the labor cost is reduced through the cutting machines.
Most of machine head trolleys of the existing cutting devices are driven by a cross beam belt to translate along the length direction of the cross beam. But if the tension of the belt of the cross beam is insufficient, the phenomenon of slipping is easy to occur, and the uniform motion of the machine head trolley in the horizontal plane is not easy to ensure.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model provides a numerical control vibrates sword and crossbeam belt and aircraft nose dolly connection guiding mechanism thereof, this crossbeam belt and aircraft nose dolly connection guiding mechanism alleviate crossbeam belt tension not enough then the phenomenon of skidding appears easily to difficult guarantee aircraft nose dolly uniform motion in the horizontal plane
The utility model discloses a crossbeam belt and aircraft nose dolly are connected guiding mechanism's technical scheme is:
the utility model provides a crossbeam belt and aircraft nose dolly connection guiding mechanism, includes connecting plate, two fixed blocks, locating plate and adjusting bolt, two the fixed block respectively with the both ends fixed connection of crossbeam belt, the connecting plate is located between two fixed blocks, the one end and the aircraft nose of connecting plate are got off fixed connection, the connecting plate respectively with two the fixed block is followed crossbeam belt length direction cooperation, locating plate fixed connection is in on the connecting plate, adjusting bolt bolted connection is in on the locating plate, adjusting bolt's screw rod section with connecting plate screw-thread fit.
As the further improvement to the above technical scheme, be equipped with the guide post on the downside of fixed block, be equipped with on the connecting plate with guide post assorted guiding hole, the guiding hole is the slot hole that extends along crossbeam belt length direction.
As a further improvement on the above technical scheme, the fixed block is kept away from the one end of connecting plate be equipped with the level to the mounting groove that the fixed block inboard extends, the tank bottom of mounting groove be equipped with the tooth's socket of taking the tooth assorted of crossbeam belt, be equipped with the clamp bolt who is used for compressing tightly the crossbeam belt on the fixed block.
As a further improvement to the technical scheme, the connection adjusting mechanism further comprises guide rails and sliding strips, the guide rails are horizontally arranged along the cross beam, the sliding strips are fixedly arranged on the lower portion of the machine head trolley and are arranged on the guide rails in a sliding mode, and the guide rails and the sliding strips are two groups of guide rails and sliding strips which are arranged in parallel at intervals on the upper sides.
The utility model discloses a technical scheme of numerical control vibration sword is:
the utility model provides a numerical control vibrates sword, includes aircraft nose dolly and crossbeam, the aircraft nose dolly is located crossbeam one side and follows the motion of crossbeam length direction, and the crossbeam belt is rectangular form, just winds the crossbeam is the annular, numerical control vibrates the sword and still includes the crossbeam belt and is connected guiding mechanism with the aircraft nose dolly, it includes connecting plate, two fixed blocks, locating plate and adjusting bolt to connect guiding mechanism, two the fixed block respectively with the both ends fixed connection of crossbeam belt, the connecting plate is located between two fixed blocks, the one end and the aircraft nose fixed connection of getting off of connecting plate, the connecting plate respectively with two the fixed block is followed crossbeam belt length direction cooperation, locating plate fixed connection be in on the connecting plate, adjusting bolt bolted connection be in on the locating plate, adjusting bolt's screw rod section with connecting plate screw-thread fit.
As the further improvement to above-mentioned technical scheme, be equipped with the guide post on the downside of fixed block, be equipped with on the connecting plate with guide post assorted guiding hole, the guiding hole is the slot hole that extends along crossbeam belt length direction.
As a further improvement on the above technical scheme, the fixed block is kept away from the one end of connecting plate be equipped with the level to the mounting groove that the fixed block inboard extends, the tank bottom of mounting groove be equipped with the tooth's socket of taking the tooth assorted of crossbeam belt, be equipped with the clamp bolt who is used for compressing tightly the crossbeam belt on the fixed block.
As a further improvement to the technical scheme, the connection adjusting mechanism further comprises guide rails and sliding strips, the guide rails are horizontally arranged along the cross beam, the sliding strips are fixedly arranged on the lower portion of the machine head trolley and are arranged on the guide rails in a sliding mode, and the guide rails and the sliding strips are two groups of guide rails and sliding strips which are arranged in parallel at intervals on the upper sides.
The utility model provides a numerical control vibrates sword and crossbeam belt and aircraft nose dolly connection guiding mechanism thereof compares in prior art, and its beneficial effect lies in:
the utility model discloses a reliable fixed connection of aircraft nose dolly and crossbeam belt is made to connecting plate, fixed block to easy dismounting.
The utility model discloses a one of them fixed block is provided with the locating plate, and two fixed blocks are fixed to crossbeam belt tip, through rotating the adjusting bolt on the locating plate, can the accurate relative position of fine setting aircraft nose dolly and crossbeam belt to make crossbeam belt tensioning.
Drawings
FIG. 1 is a diagram illustrating the usage of the present invention;
fig. 2 is an enlarged view of a portion a in fig. 1 according to the present invention;
FIG. 3 is a schematic structural view of the present invention;
fig. 4 is a schematic structural view of the fixing block of the present invention;
in the figure: 1. a cross beam; 2. a machine head trolley; 3. a cross-beam belt; 4. a connecting plate; 5. a fixed block; 6. positioning a plate; 7. a guide rail; 8. and (4) a slide bar.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and specific embodiments:
the utility model discloses a concrete embodiment of 1 felt of numerical control vibration sword crossbeam presss from both sides, as shown in fig. 1 to 4, including connecting plate 4, two fixed blocks, locating plate 6 and adjusting bolt, two fixed blocks respectively with crossbeam belt 3's both ends fixed connection, connecting plate 4 is located between two fixed blocks, the one end and the aircraft nose fixed connection of getting off of connecting plate 4, connecting plate 4 respectively with two fixed blocks along crossbeam belt 3 length direction cooperation, 6 fixed connection of locating plate are on connecting plate 4, adjusting bolt bolted connection is on locating plate 6, adjusting bolt's screw rod section and 4 screw-thread fit of connecting plate.
In this embodiment, be equipped with the guide post on the downside of fixed block, be equipped with on the connecting plate 4 with guide post assorted guiding hole, the guiding hole is the slot hole that extends along 3 length directions of crossbeam belt. The one end that the connecting plate 4 was kept away from to the fixed block is equipped with the level and to the inboard mounting groove that extends of fixed block, and the tank bottom of mounting groove is equipped with the tooth's socket that takes the tooth assorted with crossbeam belt 3, is equipped with the housing bolt who is used for compressing tightly crossbeam belt 3 on the fixed block. The connecting and adjusting mechanism further comprises a guide rail 7 and a sliding strip 8, the guide rail 7 is horizontally arranged along the cross beam 1, the sliding strip 8 is fixedly arranged on the lower portion of the machine head trolley 2 and is arranged on the guide rail 7 in a sliding mode, and the guide rail 7 and the sliding strip 8 are two groups of guide rails with upper sides arranged in parallel at intervals.
The utility model discloses a connecting plate 4, fixed block 5 make the reliable fixed connection of aircraft nose dolly 2 and crossbeam belt 3 to easy dismounting. The utility model discloses a one of them fixed block 5 is provided with locating plate 6, and two fixed blocks 5 are fixed to 3 tip of crossbeam belt, through rotating the adjusting bolt on the locating plate 6, can accurate fine setting aircraft nose dolly 2 and crossbeam belt 3's relative position to make the tensioning of crossbeam belt 3.
The utility model discloses a concrete embodiment of 1 felt of numerical control vibration sword crossbeam presss from both sides, as shown in fig. 1 to 4, including aircraft nose dolly 2 and crossbeam 1, aircraft nose dolly 2 is located crossbeam 1 one side and moves along 1 length direction of crossbeam, crossbeam belt 3 is rectangular form, and be the annular around crossbeam 1, numerical control vibration sword still includes crossbeam belt 3 and aircraft nose dolly 2 connection guiding mechanism, it includes connecting plate 4 to connect guiding mechanism, two fixed blocks, locating plate 6 and adjusting bolt, two fixed blocks respectively with crossbeam belt 3's both ends fixed connection, connecting plate 4 is located between two fixed blocks, connecting plate 4's one end and aircraft nose get off fixed connection, connecting plate 4 respectively with two fixed blocks along 3 length direction guide cooperation of crossbeam belt, 6 fixed connection of locating plate is on connecting plate 4, adjusting bolt connects on locating plate 6, adjusting bolt's screw rod section and 4 screw-thread fit of connecting plate.
In this embodiment, be equipped with the guide post on the downside of fixed block, be equipped with on the connecting plate 4 with guide post assorted guiding hole, the guiding hole is the slot hole that extends along 3 length direction of crossbeam belt. The one end that connecting plate 4 was kept away from to the fixed block is equipped with the level and to the mounting groove that the fixed block inboard extends, the tank bottom of mounting groove be equipped with the tooth's socket that takes the tooth assorted of crossbeam belt 3, be equipped with on the fixed block to be used for the housing bolt who compresses tightly crossbeam belt 3. The connecting and adjusting mechanism further comprises a guide rail 7 and a sliding strip 8, the guide rail 7 is horizontally arranged along the cross beam 1, the sliding strip 8 is fixedly arranged on the lower portion of the machine head trolley 2 and is arranged on the guide rail 7 in a sliding mode, and the guide rail 7 and the sliding strip 8 are two groups of guide rails with upper sides arranged in parallel at intervals.
The utility model discloses a connecting plate 4, fixed block 5 make the reliable fixed connection of aircraft nose dolly 2 and crossbeam belt 3 to easy dismounting. The utility model discloses a one of them fixed block 5 is provided with locating plate 6, and two fixed blocks 5 are fixed to 3 tip of crossbeam belt, through rotating the adjusting bolt on the locating plate 6, can accurate fine setting aircraft nose dolly 2 and crossbeam belt 3's relative position to make the tensioning of crossbeam belt 3.
The above description is only a preferred embodiment of the present invention, and should not be construed as limiting the present invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention should be included within the protection scope of the present invention.
Claims (8)
1. The utility model provides a crossbeam belt and aircraft nose dolly connection guiding mechanism, its characterized in that, includes connecting plate, two fixed blocks, locating plate and adjusting bolt, two the fixed block respectively with the both ends fixed connection of crossbeam belt, the connecting plate is located between two fixed blocks, the one end and the aircraft nose of connecting plate get off fixed connection, the connecting plate is followed with two the fixed block respectively crossbeam belt length direction guide cooperation, locating plate fixed connection is in on the connecting plate, adjusting bolt bolted connection is in on the locating plate, adjusting bolt's screw section with connecting plate screw-thread fit.
2. The adjusting mechanism for connecting a cross beam belt and a machine head trolley as claimed in claim 1, wherein a guide post is arranged on the lower side surface of the fixing block, a guide hole matched with the guide post is arranged on the connecting plate, and the guide hole is a long hole extending along the length direction of the cross beam belt.
3. The adjusting mechanism for connecting a cross beam belt and a machine head trolley as claimed in claim 2, wherein one end of the fixing block, which is far away from the connecting plate, is provided with a mounting groove which horizontally extends towards the inner side of the fixing block, the bottom of the mounting groove is provided with a tooth socket matched with the teeth of the cross beam belt, and the fixing block is provided with a compression bolt for compressing the cross beam belt.
4. The adjusting mechanism for connecting the cross beam belt and the machine head trolley as claimed in claim 3, further comprising a guide rail and a slide bar, wherein the guide rail is horizontally arranged along the cross beam, the slide bar is fixedly arranged at the lower part of the machine head trolley and is slidably arranged on the guide rail, and the guide rail and the slide bar are respectively two groups of guide rails and slide bars which are arranged in parallel at intervals at the upper side.
5. The utility model provides a numerical control vibrates sword, includes aircraft nose dolly and crossbeam, the aircraft nose dolly is located crossbeam one side and follows the motion of crossbeam length direction, and the crossbeam belt is rectangular form, and winds the crossbeam is the annular, a serial communication port, the numerical control vibrates sword still includes crossbeam belt and aircraft nose dolly connection guiding mechanism, it includes connecting plate, two fixed blocks, locating plate and adjusting bolt, two to connect guiding mechanism the fixed block respectively with the both ends fixed connection of crossbeam belt, the connecting plate is located between two fixed blocks, the one end of connecting plate and the aircraft nose fixed connection of getting off, the connecting plate respectively with two the fixed block is followed crossbeam belt length direction cooperation, locating plate fixed connection be in on the connecting plate, adjusting bolt bolted connection be in on the locating plate, adjusting bolt's screw rod section with connecting plate screw-thread fit.
6. The numerical control vibration knife according to claim 5, characterized in that a guide post is arranged on the lower side surface of the fixed block, a guide hole matched with the guide post is arranged on the connecting plate, and the guide hole is a long hole extending along the length direction of the beam belt.
7. The numerical control vibrating knife according to claim 6, wherein one end of the fixed block, which is far away from the connecting plate, is provided with a mounting groove extending horizontally towards the inner side of the fixed block, the bottom of the mounting groove is provided with a tooth groove matched with the teeth of the cross beam belt, and the fixed block is provided with a compression bolt for compressing the cross beam belt.
8. The numerical control vibrating knife according to claim 7, wherein the connection adjusting mechanism further comprises guide rails and sliding strips, the guide rails are horizontally arranged along the cross beam, the sliding strips are fixedly arranged at the lower part of the machine head trolley and are arranged on the guide rails in a sliding manner, and the guide rails and the sliding strips are two groups of guide rails and sliding strips which are arranged in parallel at intervals at the upper sides.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221368560.9U CN217802060U (en) | 2022-06-02 | 2022-06-02 | Numerical control vibration knife and crossbeam belt and aircraft nose dolly connection guiding mechanism thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221368560.9U CN217802060U (en) | 2022-06-02 | 2022-06-02 | Numerical control vibration knife and crossbeam belt and aircraft nose dolly connection guiding mechanism thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217802060U true CN217802060U (en) | 2022-11-15 |
Family
ID=83988651
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221368560.9U Active CN217802060U (en) | 2022-06-02 | 2022-06-02 | Numerical control vibration knife and crossbeam belt and aircraft nose dolly connection guiding mechanism thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217802060U (en) |
-
2022
- 2022-06-02 CN CN202221368560.9U patent/CN217802060U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201056655Y (en) | Yarn stitching machine | |
| CN215792688U (en) | Pneumatic marking machine capable of automatically replacing marking needle | |
| CN217802060U (en) | Numerical control vibration knife and crossbeam belt and aircraft nose dolly connection guiding mechanism thereof | |
| CN207952286U (en) | A kind of lug apparatus for bending | |
| CN207496014U (en) | The scraper power transmission that a kind of SLA3D printers are centrally located | |
| CN210500594U (en) | Eraser punching and cutting equipment | |
| CN209408586U (en) | A kind of light bar cutting equipment for LED light production | |
| CN105870753B (en) | A kind of positive-displacement machines | |
| CN207757753U (en) | A kind of die-cutting machine | |
| CN211417026U (en) | Sectional insulator mounting and adjusting tool | |
| CN206169392U (en) | Solar energy component frame double head saw | |
| CN214293485U (en) | A tooth machine is made to broad width for industry conveyer belt | |
| CN215145179U (en) | Remove and chase after and cut device | |
| CN209971158U (en) | Hydraulic plate shearing machine for production of blast furnace anhydrous stemming | |
| CN211005882U (en) | Material pressing and feeding device and sewing equipment | |
| CN218313691U (en) | Cutting mechanism and feeding device | |
| CN210518065U (en) | Upper clamping device of automatic upper clamping machine for motor rotor shaft | |
| CN211958211U (en) | Carbon brush integrated forming equipment for improving product quality | |
| CN216514802U (en) | Cloth cutting mechanism | |
| CN220373370U (en) | Cutting device for glass fiber reinforced plastic pultrusion profile | |
| CN215241037U (en) | Compression roller cuts integrative device | |
| CN213104229U (en) | Guillootine is used in fiber connector production | |
| CN212102883U (en) | Man-machine dual-purpose convenient leather cutting device | |
| CN210146762U (en) | High-speed punching device | |
| CN214819327U (en) | Automatic clamping device for full-automatic photo frame nailing machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |